Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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7 reports

Characteristics of High Performance Ejectors

Author(s): J. E. Minardi
Corporate Author: University of Dayton Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-01-01
Report Number: AFWAL TR 81-3170
full text available

Background Information and User Guide for MIL-F-8785C, Military Specification - Flying Qualities of Piloted Airplanes

Author(s): David J. Moorhouse; Robert J. Woodcock
Corporate Author: Control Dynamics Branch, Flight Control Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-07-01
Report Number: AFWAL TR 81-3109
full text available

Lateral Flying Qualities of Highly Augmented Fighter Aircraft

Author(s): Stephen J. Monagan; Rogers E. Smith; Randall E. Bailey
Corporate Author: Calspan Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-06
Report Number: AFWAL TR 81-3171 Volume 1
full text available

Lateral Flying Qualities of Highly Augmented Fighter Aircraft

Author(s): Stephen J. Monagan; Rogers E. Smith; Randall E. Bailey
Corporate Author: Calspan Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-06
Report Number: AFWAL TR 81-3171 Volume 2
full text available

A Graphic Method for Predicting Audibility of Noise Sources

Author(s): Sanford Fidell;Richard Horonjeff
Corporate Author: Bolt Beranek and Newman Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-0-01
Report Number: AFWAL TR 82-3086
full text available

Elements of Simulation Error Analysis

Author(s): Whitbeck, Richard F.
Corporate Author: Systems Technology, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-06
Report Number: AFWAL-TR-82-3022
full text by request

Proposed MIL Standard and Handbook - Flying Qualities of Air Vehicles Volume I: Proposed MIL Standard

Author(s): Ho, Roger H., David G. Mitchell, Irving L. Ashkenas, Richard H. Klein and Robert K. Heffley
Corporate Author: Systems Technology, Inc. and McDonnell Aircraft Co.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1982-11
Report Number: AFWAL-TR-82-3081 Volume I
full text by request